EP2631050B1 - Procédé et dispositif destinés à produire une matière première composite - Google Patents
Procédé et dispositif destinés à produire une matière première composite Download PDFInfo
- Publication number
- EP2631050B1 EP2631050B1 EP12001195.2A EP12001195A EP2631050B1 EP 2631050 B1 EP2631050 B1 EP 2631050B1 EP 12001195 A EP12001195 A EP 12001195A EP 2631050 B1 EP2631050 B1 EP 2631050B1
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- EP
- European Patent Office
- Prior art keywords
- semi
- finished
- webs
- semifinished
- web
- Prior art date
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- 239000002131 composite material Substances 0.000 title claims description 33
- 238000000034 method Methods 0.000 title claims description 11
- 239000000835 fiber Substances 0.000 claims description 26
- 239000000853 adhesive Substances 0.000 claims description 12
- 230000001070 adhesive effect Effects 0.000 claims description 12
- 238000004519 manufacturing process Methods 0.000 claims description 10
- 239000011159 matrix material Substances 0.000 claims description 6
- 239000004033 plastic Substances 0.000 claims description 6
- 229920003023 plastic Polymers 0.000 claims description 6
- 239000002904 solvent Substances 0.000 claims description 6
- 230000009471 action Effects 0.000 claims description 2
- 238000003825 pressing Methods 0.000 claims description 2
- 239000000126 substance Substances 0.000 claims description 2
- 239000011265 semifinished product Substances 0.000 description 54
- 239000013067 intermediate product Substances 0.000 description 9
- 239000010410 layer Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 5
- 238000004804 winding Methods 0.000 description 5
- 239000002184 metal Substances 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 238000005304 joining Methods 0.000 description 3
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 239000011151 fibre-reinforced plastic Substances 0.000 description 2
- 239000002985 plastic film Substances 0.000 description 2
- 229920006255 plastic film Polymers 0.000 description 2
- 238000002604 ultrasonography Methods 0.000 description 2
- 239000004831 Hot glue Substances 0.000 description 1
- 239000002390 adhesive tape Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000004069 differentiation Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000012815 thermoplastic material Substances 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
- B29C70/202—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/52—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
- B29C66/72141—Fibres of continuous length
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
- B29C66/73921—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
- B29C66/834—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools moving with the parts to be joined
- B29C66/8341—Roller, cylinder or drum types; Band or belt types; Ball types
- B29C66/83411—Roller, cylinder or drum types
- B29C66/83413—Roller, cylinder or drum types cooperating rollers, cylinders or drums
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2793/00—Shaping techniques involving a cutting or machining operation
- B29C2793/0081—Shaping techniques involving a cutting or machining operation before shaping
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/10—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using hot gases (e.g. combustion gases) or flames coming in contact with at least one of the parts to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/10—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using hot gases (e.g. combustion gases) or flames coming in contact with at least one of the parts to be joined
- B29C65/103—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using hot gases (e.g. combustion gases) or flames coming in contact with at least one of the parts to be joined direct heating both surfaces to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
- B29C65/1403—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the type of electromagnetic or particle radiation
- B29C65/1412—Infrared [IR] radiation
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
- B29C65/1429—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the way of heating the interface
- B29C65/1432—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the way of heating the interface direct heating of the surfaces to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
- B29C65/16—Laser beams
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4895—Solvent bonding, i.e. the surfaces of the parts to be joined being treated with solvents, swelling or softening agents, without adhesives
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5042—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like covering both elements to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/52—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive
- B29C65/524—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive by applying the adhesive from an outlet device in contact with, or almost in contact with, the surface of the part to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/114—Single butt joints
- B29C66/1142—Single butt to butt joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/116—Single bevelled joints, i.e. one of the parts to be joined being bevelled in the joint area
- B29C66/1162—Single bevel to bevel joints, e.g. mitre joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
- B29C66/435—Making large sheets by joining smaller ones or strips together
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0872—Prepregs
- B29K2105/0881—Prepregs unidirectional
Definitions
- the invention relates to a method for producing a composite material.
- the invention relates to an apparatus for producing a composite material.
- components made of fiber-reinforced plastic are used.
- Components made of fiber-reinforced plastic have the advantage of higher specific mechanical properties than metal components.
- plastics can also be used in areas where metals would corrode.
- EP 2 301 735 A2 shows a semifinished product and a semi-finished composite and manufacturing method for this semi-finished product.
- This composite then forms a kind of "sheet metal" that can be reshaped like a metal sheet.
- This semi-finished product has a relatively high tensile strength in the direction in which the fibers extend. In a direction transverse to the longitudinal extent of the fibers, the tensile strength is significantly lower. In order to increase the tensile strength, arranging several such semi-finished products one above the other, wherein the angular positions of the fibers differ from each other.
- Another way to produce a semi-finished product with increased tensile strength in several directions is to produce a so-called multi-axial web.
- EP 1 719 609 A2 shows a method and apparatus for producing a composite web based on at least two webs.
- two webs are fed parallel to a positioning zone.
- the two tracks lie next to each other.
- Another web is fed at a right angle to the first two webs, however, segments must be cut from this web before reaching the positioning zone.
- the length of these segments corresponds to the sum of the widths of the two webs.
- the segments and the webs are then joined together to form a composite web that can be wound up on a roll.
- US 2009/0301642 A1 shows a similar approach.
- a first semifinished product web is fed transversely to a second semifinished product web.
- the first semifinished sheet has reinforcing fibers which run parallel to the longitudinal direction of the semifinished sheet, ie enclose an angle of 0 °.
- the semifinished sheet has fibers which also enclose an angle of 0 ° with the longitudinal direction of the semifinished sheet.
- a multiaxial layer is created by stacking UD tracks at different angles (0 °, plus 60 °, minus 60 °).
- US Pat. No. 4,875,959 describes a method and apparatus for making a tire. Be here Elements of a rim tape laid one on top of the other and connected together on a drum.
- FR 1 362 190 A shows the production of sleeves for pneumatic bands of individual pieces, which are formed into a ring.
- WO 2012/096696 A1 shows a composite material and a method and an apparatus for its production.
- the composite is composed of modules, each of which has at least two layers of differently oriented fibers.
- US 4,708,761 A describes a device for laminating prepreg materials. These materials are unwound from rolls arranged side by side. The prepreg materials are pulled onto a support table which is laterally movable so that this support table can be positioned in front of each roller. The webs that have been removed from the rolls are deposited on the support table and then laminated together. The webs are either single-layer webs with a fiber direction of 0 ° or multi-layer webs, in which one layer has a fiber direction of 0 ° and other layers different directions of fiber.
- AT 397 062 B shows a method for the production of moldings from a plurality of oriented plastic films and a system for carrying out the method.
- molded body made of a plurality of superposed and pressed together oriented plastic films.
- the invention has for its object to facilitate the production of multiaxially reinforced materials.
- the object is achieved by a method for producing a composite material having the features of claim 1.
- the semi-finished sheets can be fed in each case in their longitudinal direction, comparatively little space is required. Also, the control of the supply of the webs can be made simple, because you do not have to make complicated conversions, in which the angle of supplied fibers or yarn sheets must be considered.
- At least two semi-finished sheets have different predetermined angles. If you use more than two semi-finished sheets, of course, two of these semi-finished sheets can also have the same angle. However, the angles of at least two semifinished sheets differ so that increased tensile strength can be achieved in at least two directions.
- the semifinished sheets are bonded together under the influence of temperature.
- the application of an elevated temperature is usually easily possible.
- the increase in temperature may, for example, soften the surface of at least one semifinished product web so that it becomes tacky and adheres to another semifinished product web.
- a connection is made between two adjacent semifinished webs before another semifinished web is added. If, for example, a first semifinished product web and a second semifinished product web are stacked on top of each other, then these two semifinished product webs can be joined together before a third semifinished product web is laid onto the second semifinished product web. The third semifinished web is then joined to the second semifinished web before the fourth semifinished web is laid up and so on.
- this has considerable advantages, because the heat must penetrate only one semifinished sheet.
- connection aids are arranged in the intermediate spaces between the semifinished product webs.
- the connection aids prepare the surfaces of the semifinished product webs such that they can be connected to the adjacent semifinished product webs.
- the semifinished webs are wound off rollers whose axes of rotation are aligned parallel to one another. You can then arrange these roles in the longitudinal direction one behind the other. To produce the composite material, it is then only necessary to unwind or pull off the semifinished product webs from the rolls. In many cases, this does not even require a drive of the rollers. The control is kept relatively simple.
- the semi-finished sheets are welded or glued together, for example.
- the bonding can be accomplished by introducing an adhesive between the adjacent semi-finished sheets, which then connects the two adjacent semi-finished sheets together.
- a solvent which dissolves the surface of at least one semifinished sheet so as to join the surface of the adjacent semifinished sheet.
- the type of connection depends, of course, on the plastic or matrix material of the semifinished product webs used.
- the semifinished sheets are joined together under pressure.
- the pressure action can be used simultaneously to calibrate the composite.
- the object is also achieved by a device for producing a composite material with the features of claim 7.
- At least two of the semi-finished sheets have different predetermined angles.
- Such a device can be used to produce a composite material which has at least two fiber layers with different angles to the longitudinal direction. Accordingly, this composite has increased tensile strength in the two directions of the fiber layers.
- At least one output device has a supply roll.
- the semifinished sheet can then be unwound from this supply roll. This facilitates stockpiling.
- At least two dispensing devices each have a supply roll and the axes of the supply rolls are aligned parallel to each other. You can then arrange these roles in the longitudinal direction one behind the other or one above the other. For producing the composite material, it is then only necessary to unwind or strip the semifinished product webs from the supply rolls. A diversion is not essential.
- connection device has a heat source.
- the heat source may be used to increase the temperature of at least one semifinished sheet. Depending on the desired connection between adjacent semifinished sheets, the temperature can then be made so high that adjacent semi-finished sheets are welded together.
- the connecting device has a dispenser for adhesive and / or solvent.
- the adhesive may then be used to bond adjacent semi-finished webs together. If a solvent is used which solubilizes the surface of the semifinished sheet, then this solvent can be applied and the then dissolved surfaces joined together. Some adhesives also stick better when the opposite surface has been pretreated with a solvent. Some adhesives also stick better or faster when heat is applied.
- a pressure device which presses at least two semifinished sheets for joining each other. Increased pressure usually leads to an improved adhesive bond.
- the pressure device has at least one roller pair.
- the roller pair then forms a nip through which the composite, i. the stack of at least two semi-finished sheets, is passed.
- Fig. 1 shows in highly schematic form a semifinished product web 1, which has a symbolized by an arrow longitudinal direction 2 and a plurality of unidirectionally directed defined fibers 3.
- the fibers 3 extend at a predetermined angle a to the longitudinal direction 2.
- a supply sheet 4 is used.
- the supply track 4 can be unwound, for example, from a supply roll 5.
- a plurality of supply rolls 5 next to one another and, correspondingly, to pull off a plurality of supply sheets 4 at the same time.
- the supply track 4 can also be generated online.
- the supply track 4 can, if appropriate already in the form of segments, also be removed from a storage or magazine.
- the web of a semi-finished product can be used as Vorratsbahn, the in EP 2 301 735 A2 is described.
- the supply track 4 may comprise a plurality of unidirectionally directed defined fibers 6, which are arranged between two layers of thermoplastic material. Another structure is of course conceivable. However, the supply track 4 has a matrix of a plastic, which holds the fibers 6 in their unidirectionally directed orientation.
- the supply track 4 has a main direction 7 marked by an arrow.
- the main direction 7 is the "longitudinal direction" of the supply track 4.
- the term “main direction” is used for differentiation purposes.
- the fibers 6 are aligned in the direction of the main direction 7, ie they are parallel to the main direction 7, wherein the term “parallel” is not to be understood in the mathematically strict sense.
- Fig. 1 How out Fig. 1 can be seen, 4 segments 8 are separated from the supply track. Each segment has two longitudinal edges 9, 10. These longitudinal edges are directed parallel to the main direction and thus parallel to the fibers 6. The longitudinal edges are at the predetermined angle a to the longitudinal direction of the second
- a separator 11 is used to separate the segments 8. This separating device cuts through the supply track 4, for example with the aid of ultrasound, with a knife, with a pair of scissors, with a band knife or with a fall knife or a guillotine.
- the separating device 11 generates a dividing line 12, which is directed parallel to the longitudinal direction 2.
- the supply track 4 is fed at an angle a to the longitudinal direction 2.
- the separating device 11 separates the segments 8 with a length of their longitudinal edges 9, 10, which corresponds to a width B of the semifinished product divided by the cosine of the angle ⁇ .
- the longitudinal edges 9, 10 are therefore longer than the width B of the semifinished product web 1. However, they are just as large that the segments 8 can later be combined to form the semifinished product web having the desired width B.
- the segments 8 can also be taken from a magazine or a store in which they have previously been stored.
- the segments 8 are stored one after another on a conveyor, not shown, and conveyed in the longitudinal direction 2. As soon as enough space is available, the next segment 8 is deposited on the conveyor.
- the representation in Fig. 1 Figure 8 shows the segment 8 separated from the semifinished sheet 1. This illustration was chosen to simplify the explanation. In fact, the segment is placed after the already finished semi-finished sheet 1.
- the semifinished product web 1 itself forms the conveyor, i. by a train on the semifinished product 1 space for the next segment 8 is created.
- connection of adjacent segments 8 at their longitudinal edges 9, 10 can be done in different ways.
- the longitudinal edges 9, 10 may be placed abutting each other and welded together by the application of heat or ultrasound. It is also possible to use a band overlapping the longitudinal edges 9, 10, which band is formed from the same material as the matrix material of the supply track 4, and then weld or glue this band to the segments 8. It is also possible to use an adhesive tape or to bond the abutting longitudinal edges 9, 10 directly to one another. You can do this, for example use a hot glue. Adjacent segments 8 can also be overlapped in the region of their longitudinal edges and then melt together. For heat supply common sources, such as laser, hot air or infrared radiation are possible.
- a connecting device 13 which can be guided in the direction of a double arrow 14 on the semifinished product web 1, ie over the two longitudinal edges 9, 10 of adjacent segments 8.
- a pressure device 15 which in the direction of a double arrow 16 can be guided over the semifinished product web 1.
- the connecting device 13 and the pressure device 15 can be operated separately or together. In the latter case, they can also be designed as a common assembly.
- the connecting device 13 can be displaced during the joining of adjacent segments 8 in the longitudinal direction 2 when the transport device is moved continuously in order to convey the semifinished product web 1 continuously.
- the connecting device 13 (the same applies, of course, for the pressure device 15) but can also be kept stationary in the longitudinal direction 2 when the conveyor is actuated in cycles.
- the semifinished sheet 1 can be wound into a winding roll 18 to facilitate its handling.
- Fig. 2 shows in highly schematic form a device 19 for producing a composite material 20.
- the composite material 20 is formed in this case by five semi-finished sheets 1a-1e, which are unwound from five winding rolls 18a-18e. A different number of semi-finished sheets is of course possible.
- the winding rolls 18a-18e have axes of rotation aligned parallel to each other, so that the individual semi-finished sheets la-le can also be fed parallel to one another.
- the bonding can be effected, for example, by applying an adhesive to one or both semifinished product webs before the semifinished product webs are placed on one another. It is also possible to soften one or both semifinished sheets on their surfaces by heat or chemical means so that they will bond together after laying, optionally by applying pressure.
- Heat may also be passed through a semifinished sheet after it has been brought into abutment with another semifinished sheet to effect welding. This heat application should be done before a another semi-finished sheet is applied, so that the heat must penetrate only a single semifinished sheet.
- Fig. 2 shows the various possibilities for interconnecting semifinished product webs.
- an adhesive applicator 21 is provided, with the adhesive is applied to the side of the semifinished sheet 1 b, which is brought to bear against the semifinished sheet 1 a.
- a first intermediate product 22 of the composite material 20 which is composed of two semi-finished sheets 18a, 18b.
- a heating device 23 is provided, which heats the semifinished product web 1c on the side facing the intermediate product 22 and makes that side so sticky that it adhere to the intermediate product 22, the is formed from the semi-finished sheets 1a, 1b, adheres.
- a further heating device 24 may be provided which heats the upper side of the intermediate product 22 facing the semifinished product web 1c in order to improve the adhesion or welding of the semifinished product web 1c to the intermediate product 22.
- a welding device 25 is provided with which the heat necessary for welding can be introduced into the semifinished product web 1d. This heat penetrates this semi-finished sheet 1d and heats it such that it is welded to an intermediate product 26 composed of the semifinished product webs 1a, 1b, 1c.
- the intermediate product 26 together with the semifinished product web 1d forms an intermediate product 27 which, together with the semifinished product web 1d, is passed through a nip formed between two pressure rollers 28, 29.
- the pressure applied there optionally after applying an adhesive to the semifinished product web 1e or a corresponding preparation, connects the semifinished product web 1e with the intermediate product 27 in order to form the composite material 20.
- connection types were listed here by way of example only. In many cases, it will be expedient to connect all semi-finished sheets 1a, 1b, 1c in the same way. If different connection types are selected, a different order of connection types is possible.
- At least two of the five semi-finished sheets 1a-1e have different angles a between the unidirectionally directed ones Fibers 3 and the longitudinal direction 2. In many cases, it will be favorable to provide all five semifinished sheets 1a-1e with different angles a of the fibers.
- the device 19 is relatively simple. You can in principle use several similar modules. Since these modules can be arranged one behind the other, relatively little space is required.
- the composite material 20 can also be produced in such a way that the semifinished product sheets 1a-1e are gathered in a fan-shaped manner from the side, heating fields being provided in the spaces between the individual semifinished product sheets 1a, 1e which, for example, due to radiant heat or contact heat Heat surfaces of the semifinished sheets 1a-1e.
- adhesive application devices may be provided in the interstices. In both cases, all the semi-finished sheets 1a-1e are simultaneously pressed against each other and thus joined to form the composite material 20.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Laminated Bodies (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
Claims (11)
- Procédé de production d'un matériau composite, selon lequel on déroule au moins deux bandes de produits semi-finis (1a-1e) à partir de rouleaux (18a-18e) dont les axes de rotation sont dirigés parallèlement les uns aux autres et qui sont agencés les uns derrière les autres ou les uns au-dessus des autres, on guide les bandes de produits semi-finis (1a-1e) parallèlement les unes aux autres dans le sens de la longueur, on les pose les unes sur les autres et on les assemble, chaque bande de produit semi-fini (1a-1e) comportant des fibres fixées dans une même direction dans une matrice plastique, les fibres d'au moins une bande de produit semi-fini formant un angle prédéterminé supérieur à 0° avec le sens de la longueur de la bande de produit semi-fini et au moins deux des bandes de produits semi-finis (1a-1e) ayant des angles différents.
- Procédé selon la revendication 1, caractérisé en ce que l'on assemble les bandes de produits semi-finis (1a-1e) sous l'action d'une température.
- Procédé selon la revendication 1 ou 2, caractérisé en ce que, en présence de plus de deux bandes de produits semi-finis (1a-1e), on effectue un assemblage entre deux bandes de produits semi-finis (1a-1b) voisines avant d'ajouter une autre bande de produit semi-fini (1e).
- Procédé selon la revendication 1 ou 2, caractérisé en ce que l'on guide ensemble au moins trois bandes de produits semi-finis (1a-1e) à la manière d'un éventail et on assemble simultanément les bandes de produits semi-finis (1a-1e).
- Procédé selon l'une des revendications 1 à 4, caractérisé en ce que l'on assemble par liaison de matière des bandes de produits semi-finis (1a-1e) voisines.
- Procédé selon l'une des revendications 1 à 5, caractérisé en ce que l'on assemble les bandes de produits semi-finis (1a-1e) sous l'action d'une pression.
- Dispositif de production d'un matériau composite (20) avec au moins deux dispositifs de sortie, chacun délivrant une bande de produit semi-fini (1a-1e) dans le sens de la longueur et les bandes de produits semi-finis (1a-1e) étant délivrées parallèlement les unes aux autres, au moins deux dispositifs de sortie comportant chacun un rouleau de réserve (18a-18e), les rouleaux de réserve étant agencés parallèlement les uns aux autres et les uns derrière les autres ou les uns au-dessus des autres, avec un dispositif d'assemblage pour assembler les bandes de produits semi-finis et avec une sortie, chaque bande de produit semi-fini (1a-1e) comportant des fibres fixées dans une même direction dans une matrice plastique et les fibres d'au moins une bande de produit semi-fini formant un angle prédéterminé supérieur à 0 ° avec le sens de la longueur de la bande de produit semi-fini (1a-1e), au moins deux des bandes de produits semi-finis (1a-1e) ayant des angles différents prédéterminés.
- Dispositif selon la revendication 7, caractérisé en ce que le dispositif d'assemblage comporte une source de chaleur.
- Dispositif selon la revendication 7 ou 8, caractérisé en ce que le dispositif d'assemblage comporte un distributeur de colle et/ou de solvant.
- Dispositif selon l'une des revendications 7 à 9, caractérisé en ce qu'il est prévu un dispositif de pression (28, 29) qui presse l'une sur l'autre pour les assembler au moins deux bandes de produits semi-finis (1a-1e).
- Dispositif selon la revendication 10, caractérisé en ce que le dispositif de pression (28, 29) comporte au moins une paire de rouleaux.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP12001195.2A EP2631050B1 (fr) | 2012-02-22 | 2012-02-22 | Procédé et dispositif destinés à produire une matière première composite |
US13/492,235 US20130213571A1 (en) | 2012-02-22 | 2012-06-08 | Method and device for producing a composite material |
JP2012151495A JP2013169793A (ja) | 2012-02-22 | 2012-07-05 | 複合材料を製造するための方法および装置 |
CN201210236753.3A CN103287049B (zh) | 2012-02-22 | 2012-07-10 | 用于制造复合材料的方法和装置 |
US14/485,304 US20150068678A1 (en) | 2012-02-22 | 2014-09-12 | Method and device for producing a composite material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP12001195.2A EP2631050B1 (fr) | 2012-02-22 | 2012-02-22 | Procédé et dispositif destinés à produire une matière première composite |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2631050A1 EP2631050A1 (fr) | 2013-08-28 |
EP2631050B1 true EP2631050B1 (fr) | 2016-07-27 |
Family
ID=45655120
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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EP12001195.2A Active EP2631050B1 (fr) | 2012-02-22 | 2012-02-22 | Procédé et dispositif destinés à produire une matière première composite |
Country Status (4)
Country | Link |
---|---|
US (2) | US20130213571A1 (fr) |
EP (1) | EP2631050B1 (fr) |
JP (1) | JP2013169793A (fr) |
CN (1) | CN103287049B (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
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KR101607362B1 (ko) * | 2012-12-21 | 2016-03-30 | (주)엘지하우시스 | 복합재료 제조 장치와, 이를 사용하여 제조되는 복합재료, 복합재료 제조 방법 |
EP2962966B1 (fr) * | 2014-07-02 | 2017-10-25 | Kiefel GmbH | Installation de fabrication d'un dispositif medical et procede de fonctionnement d'une telle installation |
WO2019046218A1 (fr) * | 2017-08-28 | 2019-03-07 | Web Industries, Inc. | Feuilles et bandes maîtresses de composite thermoplastique et procédé |
DE102017215624A1 (de) * | 2017-09-05 | 2019-03-07 | Technische Universität Dresden | Verfahren zur Herstellung von Faserverbundhalbzeugen oder Faserverbundbauteilen, Vorrichtung zur Herstellung von Faserverbundhalbzeugen oder Faserverbundbauteilen |
PL3647036T3 (pl) * | 2018-10-30 | 2023-11-06 | Profol Kunststoffe Gmbh | Zwinięta warstwa bez końca jednokierunkowo wzmocniona włóknami |
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JPS6297834A (ja) * | 1985-10-25 | 1987-05-07 | Kawasaki Heavy Ind Ltd | プリプレグ材の積層装置 |
AT397062B (de) * | 1991-08-08 | 1994-01-25 | Harald Dipl Ing Dr Schobermayr | Verfahren zur herstellung von formkörpern aus einer mehrzahl orientierter kunststoffolien und anlage zur durchführung des verfahrens |
EP2663450A1 (fr) * | 2011-01-12 | 2013-11-20 | The Board of Trustees of The Leland Stanford Junior University | Structures stratifiées composites et procédés de fabrication et d'utilisation associés |
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FR1362190A (fr) * | 1963-06-27 | 1964-05-29 | Yokohama Rubber Co Ltd | Perfectionnements apportés aux procédés de fabrication d'enveloppes pour bandages pneumatiques |
US4199635A (en) * | 1979-04-20 | 1980-04-22 | Albany International Corp. | Fabric faced laminate panel and method of manufacture |
JPH07115425B2 (ja) * | 1986-09-24 | 1995-12-13 | 株式会社ブリヂストン | タイヤ成形方法および装置 |
JPH0230518A (ja) * | 1988-07-21 | 1990-01-31 | Tonen Corp | 連続的繊維強化複合材料の製造装置 |
US5173138A (en) * | 1990-08-08 | 1992-12-22 | Blauch Denise A | Method and apparatus for the continuous production of cross-plied material |
JPH0577379A (ja) * | 1991-09-19 | 1993-03-30 | Hitachi Chem Co Ltd | 積層板の連続製造方法及び積層装置 |
BE1007230A3 (nl) * | 1993-06-23 | 1995-04-25 | Dsm Nv | Composietbaan van onderling parallelle vezels in een matrix. |
FR2761380B1 (fr) * | 1997-03-28 | 1999-07-02 | Europ Propulsion | Procede et machine pour la realisation de nappes fibreuses multiaxiales |
JP4363741B2 (ja) * | 2000-04-14 | 2009-11-11 | 本田技研工業株式会社 | 繊維強化複合材からなる中間成形物品の製造方法 |
US20040234744A1 (en) * | 2003-05-19 | 2004-11-25 | Byma George B. | Vehicle interior trim component of basalt fibers and thermoplastic binder and method of manufacturing the same |
WO2005033393A1 (fr) * | 2003-09-30 | 2005-04-14 | Fabrics Technologies Llc | Materiaux composites thermoplastiques renforces par des fibres et leur procede de fabrication |
NL1028977C2 (nl) * | 2005-05-04 | 2006-11-07 | Beiler Beheer Bv | Werkwijze en inrichting voor het vervaardigen van een samengestelde baan op basis van ten minste twee banen. |
CN100398763C (zh) * | 2005-06-30 | 2008-07-02 | 雷智斌 | 外墙保温装饰板及其制造方法 |
JP5242030B2 (ja) * | 2006-07-31 | 2013-07-24 | 宇部日東化成株式会社 | 複数組の金属箔/樹脂フィルム構造の長尺状積層体の製造法 |
US7964050B2 (en) * | 2008-06-04 | 2011-06-21 | Barrday, Inc. | Method for processing a composite |
DE102009043280A1 (de) | 2009-09-29 | 2011-03-31 | Karl Mayer Malimo Textilmaschinenfabrik Gmbh | Halbzeug und Halbzeugverbund |
-
2012
- 2012-02-22 EP EP12001195.2A patent/EP2631050B1/fr active Active
- 2012-06-08 US US13/492,235 patent/US20130213571A1/en not_active Abandoned
- 2012-07-05 JP JP2012151495A patent/JP2013169793A/ja active Pending
- 2012-07-10 CN CN201210236753.3A patent/CN103287049B/zh active Active
-
2014
- 2014-09-12 US US14/485,304 patent/US20150068678A1/en not_active Abandoned
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Publication number | Priority date | Publication date | Assignee | Title |
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JPS6297834A (ja) * | 1985-10-25 | 1987-05-07 | Kawasaki Heavy Ind Ltd | プリプレグ材の積層装置 |
AT397062B (de) * | 1991-08-08 | 1994-01-25 | Harald Dipl Ing Dr Schobermayr | Verfahren zur herstellung von formkörpern aus einer mehrzahl orientierter kunststoffolien und anlage zur durchführung des verfahrens |
EP2663450A1 (fr) * | 2011-01-12 | 2013-11-20 | The Board of Trustees of The Leland Stanford Junior University | Structures stratifiées composites et procédés de fabrication et d'utilisation associés |
Also Published As
Publication number | Publication date |
---|---|
CN103287049A (zh) | 2013-09-11 |
US20150068678A1 (en) | 2015-03-12 |
CN103287049B (zh) | 2016-01-20 |
JP2013169793A (ja) | 2013-09-02 |
US20130213571A1 (en) | 2013-08-22 |
EP2631050A1 (fr) | 2013-08-28 |
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